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基于混合优化算法的空间拦截轨道优化设计

高晓光 汤洪 端军红

高晓光, 汤洪, 端军红等 . 基于混合优化算法的空间拦截轨道优化设计[J]. 北京航空航天大学学报, 2015, 41(9): 1574-1581. doi: 10.13700/j.bh.1001-5965.2014.0673
引用本文: 高晓光, 汤洪, 端军红等 . 基于混合优化算法的空间拦截轨道优化设计[J]. 北京航空航天大学学报, 2015, 41(9): 1574-1581. doi: 10.13700/j.bh.1001-5965.2014.0673
GAO Xiaoguang, TANG Hong, DUAN Junhonget al. Space interception orbit optimization design based on hybrid optimal algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(9): 1574-1581. doi: 10.13700/j.bh.1001-5965.2014.0673(in Chinese)
Citation: GAO Xiaoguang, TANG Hong, DUAN Junhonget al. Space interception orbit optimization design based on hybrid optimal algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(9): 1574-1581. doi: 10.13700/j.bh.1001-5965.2014.0673(in Chinese)

基于混合优化算法的空间拦截轨道优化设计

doi: 10.13700/j.bh.1001-5965.2014.0673
基金项目: 国家自然科学基金(60774064)
详细信息
    通讯作者:

    高晓光(1957—),女,辽宁鞍山人,教授,cxg2012@nwpu.edu.cn,主要研究方向为航空火力控制、武器系统作战效能分析.

  • 中图分类号: V448.234;TB491

Space interception orbit optimization design based on hybrid optimal algorithm

  • 摘要: 基于改进高斯法(IGM)和遗传算法(GA)的混合优化算法,为解决空间拦截轨道燃料消耗和转移时间的综合最优问题,提出一种空间拦截轨道设计方法.首先,引入牛顿-拉夫逊迭代法对原始高斯法进行改进,解决原始高斯法在解算空间拦截轨道时收敛速度慢、转移角范围小等问题;接着,给出并证明改进高斯法迭代方程有唯一解的充分必要条件.当给定初始轨道参数时,用此条件判断可否用椭圆轨道进行转移;然后给出转移时间,最大脉冲速度等约束条件,对编码方式进行改进,给出混合优化算法的计算步骤;最后以空间拦截轨道优化问题为例,进行仿真分析.仿真结果表明,与传统优化算法相比,混合优化算法收敛的遗传代数少,耗时短,能够较好地运用于空间拦截轨道的设计.

     

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出版历程
  • 收稿日期:  2014-10-30
  • 刊出日期:  2015-09-20

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